• Title/Summary/Keyword: satellite optical observation

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Fabrication and Performance Test of Small Satellite Camera with Focus Mechanism (포커스 메커니즘이 적용된 소형 위성 카메라의 제작 및 성능 실험)

  • Hong, Dae Gi;Hwang, Jai Hyuk
    • Journal of Aerospace System Engineering
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    • v.13 no.4
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    • pp.26-36
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    • 2019
  • The precise alignment between optical components is required in high-resolution earth observation satellites. However, the misalignment of optical components occurs due to external factors such as severe satellite launch environment and space environment. A satellite optical system with a focus mechanism is required to compensate for the image quality degraded by these misalignments. This study designed, fabricated, aligned precisely, and carried out a performance tests for the image quality of the system. The satellite optical camera performance tests were carried out to check the image quality change by operating the focus mechanism and to analyze the satellite optical system MTF by photographing USAF target using the autocollimator. According to the experimental results, the misalignments can be compensated sufficiently with the focus mechanism. Finally the basic data for re-focusing algorithm of the optical system was obtained through this study.

Retrieval of LIDAR Aerosol Parameter Using Sun/Sky Radiometer at Gangneung, Korea

  • Shin, Sung-Kyun;Lee, Kwon-Ho;Lee, Kyu-Tae
    • Current Optics and Photonics
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    • v.1 no.3
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    • pp.175-185
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    • 2017
  • The aerosol optical properties such as depolarization ratio (${\delta}$) and aerosol extinction-to-backscatter ratios (S, LIDAR ratio) and ${\AA}ngstr{\ddot{o}m$ exponent (${\AA}$) derived from measurement with AERONET sun/sky radiometer at Gangneung-Wonju National University (GWNU), Gangneung, Korea ($37.77^{\circ}N$, $128.87^{\circ}E$) during a winter season (December 2014 - February 2015) are presented. The PM concentration measurements are conducted simultaneously and used to identify the high-PM events. The observation period was divided into three cases according to the PM concentrations. We analysed the ${\delta}$, S, and ${\AA}$ during these high PM-events. These aerosol optical properties are calculated by the sun/sky radiometer data and used to classify a type of aerosols (e.g., dust, anthropogenic pollution). The higher values of ${\delta}$ with lower values of S and ${\AA}$ were measured for the dust particles. The mean values of ${\delta}$, S, and ${\AA}$ at 440-870 nm wavelength pair (${\AA}_{440-870}$) for the Asia dust were 0.19-0.24, 36-56 sr, and 0.48, respectively. The anthropogenic aerosol plumes are distinguished with the lower values of ${\delta}$ and higher values of ${\AA}$. The mean values of spectral ${\delta}$ and ${\AA}_{440-870}$ for this case varied 0.06-0.16 and 1.33-1.39, respectively. We found that aerosol columnar optical properties obtained from the sun/sky radiometer measurement are useful to identify the aerosol type. Moreover, the columnar aerosol optical properties calculated based on sun/sky radiometer measurements such as ${\delta}$, S, and ${\AA}$ will be further used for the validation of aerosol parameters obtained from LIDAR observation as well as for quantification of the air quality.

Attitude Scenarios of Star Observation for Image Validation of Remote Sensing Satellite (영상검정을 위한 지구관측위성의 별 관측 자세 시나리오 생성 기법)

  • Yu, Ji-Woong;Park, Sang-Young;Lee, Dong-Han
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.9
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    • pp.807-817
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    • 2012
  • An optical payload needs to be validated its image performance after launched into orbit. The image performance was validated by observing star because ground site contains uncertainties caused by atmosphere, time of the year, and weather. Time Delayed and Integration(TDI) technique, which is mostly used to observe the ground, is going to be used to observe the selected stars. A satellite attitude scenario was also developed to observe the selected stars. The scenario is created to enable TDI to operate. Rotation angles of optical payload are determined in order for the selected stars to properly be passed at a desired angular velocity about rotation axis. The result of this research can be utilized to validate the quality of optical payload of a satellite in orbit. In addition, a quaternion for pointing selected stars is calculated minimizing the path from a given arbitrary attitude of satellite.

Aerosol Optical Thickness Measurements from the Microtops-II Multi-wavelength Radiometer (마이크로탑스 II 다파장 복사계를 이용한 대기 에어로솔 광학 두께 관측)

  • Lee, Kwon-Ho;Lee, Kyu-Tae
    • Journal of Korean Society for Atmospheric Environment
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    • v.32 no.1
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    • pp.57-66
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    • 2016
  • Aerosol optical thickness (AOT) and ${\AA}ngstr{\ddot{o}}m$ exponents were monitored at the KIU site ($N35.91^{\circ}$, $E128.80^{\circ}$) during the continuous observation period of 5 November 2010~19 March 2013 using a Microtops-II handheld munti-wavelenth radiometer. Comparisons of AOT values from the Microtops-II with the Sun-sky radiometer data from the Aerosol Robotic Network (AERONET) showed very good agreements: correlation coefficients are lies between 0.98 and 0.99, slopes range from 0.98 to 1.01, and intercepts are smaller than 0.008 at five wavelengths (380 nm, 440 nm, 500 nm, 675 nm, 870 nm). During the observation period, the Microtops-II AOT and ${\AA}ngstr{\ddot{o}}m$ exponents are ${\tau}_{500}=0.560{\pm}0.351$, ${\alpha}_{500-870}=1.135{\pm}0.445$. Fine mode aerosols appear to dominate in the study region with significant contributions from small particles.

Improving Orbit Determination Precision of Satellite Optical Observation Data Using Deep Learning (심층 학습을 이용한 인공위성 광학 관측 데이터의 궤도결정 정밀도 향상)

  • Hyeon-man Yun;Chan-Ho Kim;In-Soo Choi;Soung-Sub Lee
    • Journal of Advanced Navigation Technology
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    • v.28 no.3
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    • pp.262-271
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    • 2024
  • In this paper, by applying deep learning, one of the A.I. techniques, through angle information, which is optical observation data generated when observing satellites at observatories, distance information from observatories is learned to predict range data, thereby increasing the precision of satellite's orbit determination. To this end, we generated observational data from GMAT, reduced the learning data error of deep learning through preprocessing of the generated observational data, and conducted deep learning through MATLAB. Based on the predicted distance information from learning, trajectory determination was performed using an extended Kalman filter, one of the filtering techniques for trajectory determination, through GMAT. The reliability of the model was verified by comparing and analyzing the orbital determination with angular information without distance information and the orbital determination result with predicted distance information from the model.

Aerosol Direct Radiative Forcing by Three Dimensional Observations from Passive- and Active- Satellite Sensors (수동형-능동형 위성센서 관측자료를 이용한 대기 에어러솔의 3차원 분포 및 복사강제 효과 산정)

  • Lee, Kwon-Ho
    • Journal of Korean Society for Atmospheric Environment
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    • v.28 no.2
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    • pp.159-171
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    • 2012
  • Aerosol direct radiative forcing (ADRF) retrieval method was developed by combining data from passive and active satellite sensors. Aerosol optical thickness (AOT) retrieved form the Moderate Resolution Imaging Spectroradiometer (MODIS) as a passive visible sensor and aerosol vertical profile from to the Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observations (CALIPSO) as an active laser sensor were investigated an application possibility. Especially, space-born Light Detection and Ranging (Lidar) observation provides a specific knowledge of the optical properties of atmospheric aerosols with spatial, temporal, vertical, and spectral resolutions. On the basis of extensive radiative transfer modeling, it is demonstrated that the use of the aerosol vertical profiles is sensitive to the estimation of ADRF. Throughout the investigation of relationship between aerosol height and ADRF, mean change rates of ADRF per increasing of 1 km aerosol height are smaller at surface than top-of-atmosphere (TOA). As a case study, satellite data for the Asian dust day of March 31, 2007 were used to estimate ADRF. Resulting ADRF values were compared with those retrieved independently from MODIS only data. The absolute difference values are 1.27% at surface level and 4.73% at top of atmosphere (TOA).

The Photometric Brightness Variation of Geostationary Orbit Satellite

  • Seo, Haingja;Jin, Ho;Song, Yongjun;Lee, Yongseok;Oh, Youngseok
    • Journal of Astronomy and Space Sciences
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    • v.30 no.3
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    • pp.179-185
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    • 2013
  • Photometric observation is one of the most effective techniques for determining the physical characteristics of unknown space objects and space debris. In this research, we examine the change in brightness of the Communication, Ocean, Meteorological Satellite-1 (COMS-1) Geostationary Orbit Satellite (GEO), and compare it to our estimate model. First, we calculate the maximum brightness time using our calculation method and then derive the light curve shape using our rendering model. The maximum brightness is then calculated using the induced equation from Pogson's formula. For a comparison with our estimation, we carried out photometric observation using an optical telescope. The variation in brightness and the shape of the light curve are similar to the calculations achieved using our model, but the maximum brightness shows a slightly different value from our calculation result depending on the input parameters. This paper examines the photometric phenomenon of the variation in brightness of a GEO satellite, and the implementation of our approach to understanding the characteristics of space objects.

Design of 3-Axis Focus Mechanism Using Piezoelectric Actuators for a Small Satellite Camera (소형 위성 카메라의 압전작동기 타입 3-축 포커스 메커니즘 설계)

  • Hong, Dae Gi;Hwang, Jai Hyuk
    • Journal of Aerospace System Engineering
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    • v.12 no.3
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    • pp.9-17
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    • 2018
  • For Earth observation, a small satellite camera has relatively weak structural stability compared to medium-sized satellite, resulting in misalignment of optical components due to severe launching and space environments. These alignment errors can deteriorate the optical performance of satellite cameras. In this study, we proposed a 3-axis focus mechanism to compensate misalignment in a small satellite camera. This mechanism consists of three piezo-electric actuators to perform x-axis and y-axis tilt with de-space compensation. Design requirements for the focus mechanism were derived from the design of the Schmidt-Cassegrain target optical system. To compensate the misalignment of the secondary mirror (M2), the focus mechanism was installed just behind the M2 to control the 3-axis movement of M2. In this case, flexure design with Box-Behnken test plan was used to minimize optical degradation due to wave front error. The wave front error was analyzed using ANSYS. The fabricated focus mechanism demonstrated excellent servo performance in experiments with PID servo control.

Performance of Support Vector Machine for Classifying Land Cover in Optical Satellite Images: A Case Study in Delaware River Port Area

  • Ramayanti, Suci;Kim, Bong Chan;Park, Sungjae;Lee, Chang-Wook
    • Korean Journal of Remote Sensing
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    • v.38 no.6_4
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    • pp.1911-1923
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    • 2022
  • The availability of high-resolution satellite images provides precise information without direct observation of the research target. Korea Multi-Purpose Satellite (KOMPSAT), also known as the Arirang satellite, has been developed and utilized for earth observation. The machine learning model was continuously proven as a good classifier in classifying remotely sensed images. This study aimed to compare the performance of the support vector machine (SVM) model in classifying the land cover of the Delaware River port area on high and medium-resolution images. Three optical images, which are KOMPSAT-2, KOMPSAT-3A, and Sentinel-2B, were classified into six land cover classes, including water, road, vegetation, building, vacant, and shadow. The KOMPSAT images are provided by Korea Aerospace Research Institute (KARI), and the Sentinel-2B image was provided by the European Space Agency (ESA). The training samples were manually digitized for each land cover class and considered the reference image. The predicted images were compared to the actual data to obtain the accuracy assessment using a confusion matrix analysis. In addition, the time-consuming training and classifying were recorded to evaluate the model performance. The results showed that the KOMPSAT-3A image has the highest overall accuracy and followed by KOMPSAT-2 and Sentinel-2B results. On the contrary, the model took a long time to classify the higher-resolution image compared to the lower resolution. For that reason, we can conclude that the SVM model performed better in the higher resolution image with the consequence of the longer time-consuming training and classifying data. Thus, this finding might provide consideration for related researchers when selecting satellite imagery for effective and accurate image classification.

Technology Trends in Space Optical Communications (우주 광통신 기술 동향)

  • C.I. Yeo;Y.S. Heo;S.W. Park;K.S. Kim;H.S. Kang
    • Electronics and Telecommunications Trends
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    • v.38 no.2
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    • pp.85-95
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    • 2023
  • Space optical communication technology capable of large-capacity, high-speed, and low-latency communication can reduce the size, weight, and power consumption of radio frequency communications in existing satellite systems, thereby reducing launch costs, accommodating additional science instruments, and extending lifetime. Despite the high technical difficulty, various projects are being carried out in advanced countries regarding space technology for use in national security and defense, earth observation, and space communications. We review the advantages, key components, and development trends of space optical communication technology, which is attracting attention in applications such as satellite communications, intersatellite linking, and deep space communications.